DocumentCode
2947771
Title
UPF algorithm and its application in the GPS/INS integrated navigation
Author
Tian, Lei ; Rong, Jian ; Zhong, Xiaochun ; Li, Tao
Author_Institution
Sch. of Phys. Electron., Univ. of Electron. Sci. & Technol. of China (UESTC), Chengdu, China
fYear
2009
fDate
13-15 Nov. 2009
Firstpage
1
Lastpage
4
Abstract
The integration of position and velocity is commonly adopted for observation model in GPS/INS integrated navigation system. But the navigation accuracy of this system is decreased by the correlation between the system´s measurements. So the pseudo-range of the original measurements of GPS was adopted for observation model to eliminate the correlation. To reduce the linearization error, the unscented particle filter (UPF) was introduced to estimate the system states. The simulation was carried out under the condition of less than four GPS satellites data. The simulation results show that the estimated values with UPF method are quite close to the real values and the estimation error is much smaller than the inherent error of GPS. Both the figures and the statistical results prove that the UPF method present high navigation accuracy when employed in GPS/INS integrated navigation system.
Keywords
Global Positioning System; inertial navigation; inertial systems; statistical analysis; GPS satellites data; Global Positioning System; inertial navigation system; integrated navigation system; unscented particle filter; Calibration; Costs; Estimation error; Filtering algorithms; Global Positioning System; Inertial navigation; Mathematical model; Particle filters; Satellite navigation systems; State estimation; GPS/INS integrated navigation; observation model; pseudo-range; unscented particle filter (UPF);
fLanguage
English
Publisher
ieee
Conference_Titel
Wireless Communications & Signal Processing, 2009. WCSP 2009. International Conference on
Conference_Location
Nanjing
Print_ISBN
978-1-4244-4856-2
Electronic_ISBN
978-1-4244-5668-0
Type
conf
DOI
10.1109/WCSP.2009.5371394
Filename
5371394
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